FR3082826B1 - FIXING INTERFACE, FLOTATION SYSTEM AND VEHICLE - Google Patents

FIXING INTERFACE, FLOTATION SYSTEM AND VEHICLE Download PDF

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Publication number
FR3082826B1
FR3082826B1 FR1800660A FR1800660A FR3082826B1 FR 3082826 B1 FR3082826 B1 FR 3082826B1 FR 1800660 A FR1800660 A FR 1800660A FR 1800660 A FR1800660 A FR 1800660A FR 3082826 B1 FR3082826 B1 FR 3082826B1
Authority
FR
France
Prior art keywords
fixing interface
interface
fitting
vehicle
fixing
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
FR1800660A
Other languages
French (fr)
Other versions
FR3082826A1 (en
Inventor
Nicolas Ghirardi
Samuel Pellerin
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Helicopters Deutschland GmbH
Airbus Helicopters SAS
Original Assignee
Airbus Helicopters Deutschland GmbH
Airbus Helicopters SAS
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Airbus Helicopters Deutschland GmbH, Airbus Helicopters SAS filed Critical Airbus Helicopters Deutschland GmbH
Priority to FR1800660A priority Critical patent/FR3082826B1/en
Priority to EP19182507.4A priority patent/EP3587271B1/en
Publication of FR3082826A1 publication Critical patent/FR3082826A1/en
Application granted granted Critical
Publication of FR3082826B1 publication Critical patent/FR3082826B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D25/00—Emergency apparatus or devices, not otherwise provided for
    • B64D25/08—Ejecting or escaping means
    • B64D25/18—Flotation gear
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/54—Floats
    • B64C25/56—Floats inflatable

Abstract

La présente invention concerne une interface de fixation (1) munie d'une ferrure (10), ladite ferrure (10) comprenant au moins un organe de fixation (20) configuré pour fixer l'interface de fixation (1) à un premier élément (5) n'appartenant pas à l'interface de fixation (1), ladite interface de fixation (1) comprenant au moins une ralingue (60, 61) attachée à ladite ferrure (10). La ferrure (10) comprend au moins un support principal (25) traversé par une tige principale (35), ladite tige principale (35) étant configurée pour traverser une attache d'un deuxième élément, ce deuxième élément n'appartenant pas à l'interface de fixation (1) et étant distinct du premier élément (5). L'interface peut être configurée pour fixer un premier élément d'un conteneur à un deuxième élément d'un système de flottation à un véhicule, ladite au moins une ralingue étant relié à un flotteur.The present invention relates to a fixing interface (1) provided with a fitting (10), said fitting (10) comprising at least one fixing member (20) configured to fix the fixing interface (1) to a first element. (5) not belonging to the fixing interface (1), said fixing interface (1) comprising at least one bolt rope (60, 61) attached to said fitting (10). The fitting (10) comprises at least one main support (25) crossed by a main rod (35), said main rod (35) being configured to pass through a fastener of a second element, this second element not belonging to the 'fixing interface (1) and being separate from the first element (5). The interface can be configured to attach a first element of a container to a second element of a vehicle flotation system, said at least one bolt rope being connected to a float.

FR1800660A 2018-06-26 2018-06-26 FIXING INTERFACE, FLOTATION SYSTEM AND VEHICLE Active FR3082826B1 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1800660A FR3082826B1 (en) 2018-06-26 2018-06-26 FIXING INTERFACE, FLOTATION SYSTEM AND VEHICLE
EP19182507.4A EP3587271B1 (en) 2018-06-26 2019-06-26 Flotation system provided with an attachment interface and associated vehicle

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1800660A FR3082826B1 (en) 2018-06-26 2018-06-26 FIXING INTERFACE, FLOTATION SYSTEM AND VEHICLE
FR1800660 2018-06-26

Publications (2)

Publication Number Publication Date
FR3082826A1 FR3082826A1 (en) 2019-12-27
FR3082826B1 true FR3082826B1 (en) 2020-11-27

Family

ID=63557528

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1800660A Active FR3082826B1 (en) 2018-06-26 2018-06-26 FIXING INTERFACE, FLOTATION SYSTEM AND VEHICLE

Country Status (2)

Country Link
EP (1) EP3587271B1 (en)
FR (1) FR3082826B1 (en)

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB8927595D0 (en) * 1989-12-06 1990-02-07 Fpt Industries Inflatable buoyancy members
KR100371239B1 (en) * 2000-11-22 2003-02-07 현대자동차주식회사 Hood hinge structure of vehicle
US6709305B2 (en) * 2001-09-21 2004-03-23 Apical Industries, Inc. Floatation system including life raft
US6644592B2 (en) 2001-09-21 2003-11-11 Apical Industries, Inc. Floatation system
FR2917713B1 (en) * 2007-06-21 2009-09-25 Airbus France Sas APPARATUS FOR ATTACHING AN AIRCRAFT ENGINE AND AIRCRAFT HAVING AT LEAST ONE SUCH DEVICE.
FR2959207B1 (en) * 2010-04-26 2012-04-20 Eurocopter France ENERGY-ABSORPTION SYSTEM FOR AN ATTERISSEUR, AND AIRCRAFT PROVIDED WITH SAID ENERGY ABSORPTION SYSTEM
FR3057212B1 (en) * 2016-10-12 2018-10-05 Airbus Helicopters TRANSPARENT STRUCTURE FOR WINDOW AND AIRCRAFT

Also Published As

Publication number Publication date
FR3082826A1 (en) 2019-12-27
EP3587271A1 (en) 2020-01-01
EP3587271B1 (en) 2020-07-29

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